EP0171798B1 - Hochfester Werkstoff hergestellt durch Verfestigung rasch erstarrter Aluminiumlegierungsteilchen - Google Patents

Hochfester Werkstoff hergestellt durch Verfestigung rasch erstarrter Aluminiumlegierungsteilchen Download PDF

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Publication number
EP0171798B1
EP0171798B1 EP85110169A EP85110169A EP0171798B1 EP 0171798 B1 EP0171798 B1 EP 0171798B1 EP 85110169 A EP85110169 A EP 85110169A EP 85110169 A EP85110169 A EP 85110169A EP 0171798 B1 EP0171798 B1 EP 0171798B1
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EP
European Patent Office
Prior art keywords
aluminum alloy
aluminum
strength material
alloy
rapidly solidified
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Expired
Application number
EP85110169A
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English (en)
French (fr)
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EP0171798A1 (de
Inventor
Susumu Inumaru
Shigenori Yamauchi
Kazuhisa Shibue
Hideo Sano
Kiyofumi Ito
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Sumitomo Light Metal Industries Ltd
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Sumitomo Light Metal Industries Ltd
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Publication date
Application filed by Sumitomo Light Metal Industries Ltd filed Critical Sumitomo Light Metal Industries Ltd
Publication of EP0171798A1 publication Critical patent/EP0171798A1/de
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor

Definitions

  • the present invention relates to aluminum alloy materials produced by means of powder metallurgical technique and more particularly to formed materials having a high strength at high temperatures as well as moderate temperatures, the material being produced by consolidating aluminum alloy particulates rapidly solidified in atomization or other conventional processes into a desired configuration by extrusion, rolling, forging, sintering, hot isostatic pressing or other usual forming processes.
  • AI-Fe system alloys such as AI-8Fe-4Ce, AI-8Fe-2Co and AI-8Fe-2Mo, which are produced by the process including rapid solidification and consolidation, have been proposed as heat resistant aluminum alloys.
  • these conventional materials do not always provide satisfactory utility in the practical use.
  • the foregoing AI-8Fe-4Ce material increases the cost of the finished products because of the addition of expensive Ce.
  • the materials of AI-8Fe-2Co alloy and AI-8Fe-2Mo alloy can not always give an adequate high-temperature strength in practical use.
  • EP-A 0,136,508 discloses high strength aluminum-transition metal alloys consisting of 7 to 15 wt% Fe, at least one of V, Mo, Ni, Zr, Ti, Zn, Co, Cr, Y, Si, Ce in a range from 1.5 to 10 wt% and the balance being aluminum.
  • the object of the present invention is to eliminate the above disadvantages encountered in the heretofore known materials formed from the foregoing rapidly solidifed aluminum alloys, i.e. AI-8Fe-4Ce, AI-8Fe-2Co or AI-8Fe-2Mo. More specifically, the object of the present invention is to provide aluminum alloy materials formed from rapidly solidified aluminum alloy particulates with novel compositions, in which their strength at high temperatures is considerably increased by a fine dispersion of primary phase and/or precipitates of iron-containing intermetallic compounds having a size of not greater than 5 pm, without using expensive cerium (Ce).
  • a superior high-temperature strength aluminum alloy material which is strengthened by primary phase and/or precipitates of iron-containing intermetallic compounds with a fine size not greaterthan 5 pm, the material being produced by consolidating the rapidly solidified particulates of aluminum alloy (1) or (2) with the following novel compositions, in weight percentages, into a desired form in a usual manner.
  • Aluminum Alloy (1) at least one member of the group consisting of: the balance being aluminum and incidental impurities, said aluminum alloy being strengthened by a fine dispersion of Fe-containing inter-metallic compounds having a size of 5 pm and less.
  • Aluminum Alloy (2) the balance being aluminum and incidental impurities, said aluminum alloy being strengthened by a fine dispersion of Fe-containing intermetallic compounds having a size of 5 um and less.
  • the aluminum materials above specified exhibit a high temperature at high temperatures as well as moderate temperatures without using expensive Ce, they are highly useful as economical heat-resistant materials for various applications, particularly for the fields where high strength at high temperatures and light weight are desirable.
  • the present invention resides in the provision of high-temperature strength aluminum alloy materials not containing expensive Ce which are produced by consolidating the rapidly solidified aluminum alloy (1) or (2) having the novel composition specified above.
  • Fe-containing intermetallic compounds are dispersed in the matric as fine primary phases during rapid solidification and/or as fine precipitates during consolidation with a fine size not greater than 5 pm. Such a fine dispersion of the intermetallic compounds lead to a substantial increase in strength at elevated temperatures and moderate temperatures in the formed materials. When the Fe content is less than 4 wt.%, this effect is inadequate. On the other hand, even if Fe is contained in an excess amount over 15 wt.%, the effect can not be further increased, because it is saturated.
  • V This component refines the foregoing Fe-bearing intermetallic compounds and enhances the strengthening effect of Fe.
  • formed aluminum alloys containing V have a further increased strength at moderate temperatures and high temperatures as compared to AI-Fe binary alloys.
  • V is less than 0.5 wt.%, this effect can not be sufficiently obtained.
  • an excess addition of V beyond its upper limit, i.e. 8 wt.% can not provide any further increased effect, because the effect reaches the maximum level and unfavorably leads to an increase in cost.
  • Alloys 1 to 6 given in Table 1 were melted and rapidly solidified powders with an average diameter of 60 pm were produced by He gas atomization process.
  • the cooling rate in the process is approximately from 10 3 to 10 4 °C/sec.
  • the powders thus obtained from each alloy composition were formed into a rod shape with a diameter of 18 mm in the following procedures: cold compaction of the alloy powders until 70 to 80% of theoretical density, packing the compacted alloy powders in an aluminum can, vacuum degassing at an elevated temperature of 400°C and then extruding into a rod shape with a diameter of 18 mm.
  • a comparative alloy 7 was melted and then cast into an ingot having a diameter of 152 mm by a continuous casting process (cooling rate: less than 10°C/sec). Thereafter, the ingot was extruded into a rod with a diameter of 40 mm at 400°C and then solution heat treated for 24 hours at 530°C. After solution heat treating, the allow rod was cooled with hot water and subsequently was subjected to an aging treatment for 20 hours at 200°C (T6 type heat treatment).
  • the alloy rods thus obtained were subjected to the tensile test at room temperature and 250°C (holding time: 100 Hrs).
  • the test results are given in Table 2 in which the numbers of the alloy rods indicated in Table 2 correspond to the numbers of the alloys in Table 1, respectively.
  • the formed products 1, 2 and 3 of the present invention are superior in their mechanical strength both at room temperature and the elevated temperature to the conventional alloy products 4 to 7. Also enconomical advantages make the invention products commercially valuable and highly useful for practical uses. Further, the alloy rods according to the present invention are far superior in their strength at high temperatures as compared with alloy rod No. 7 which is made of a typical heat-resistant alloy by means of ingot metallurgy process.

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  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Continuous Casting (AREA)

Claims (5)

1. Hochfestes Material, hergestellt durch Verfestigen schnell erstarrter Partikel einer Aluminiumlegierung, wobei die Aluminiumlegierung, in Gewichtsprozenten, aus:
Figure imgb0010
mindestens einem Mitglied der Gruppe:
Figure imgb0011
und der Rest aus Aluminium und zufälligen Verunreinigungen besteht, wobei die Aluminiumlegierung durch eine feine Dispersion eisenhaltiger intermetallischer Verbindungen mit einer Größe von 5 um und winiger verfestigt ist.
2. Hochfestes Material nach Anspruch 1, bei dem die schnell erstarrten Partikel durch Atomisieren und Erstarren einer Aluminiumlegierungsschmelze bei einer Abkühlungsgeschwindigkeit von 103 bis 104°C/sec unter Verwendung eines Gases, hergestellt wurden.
3. Hochfestes Material, hergestellt durch Verfestigen schnell erstarrter Partikel einer Aluminiumlegierung, wobei die Aluminiumlegierung, in Gewichtsprozenten, aus:
Figure imgb0012
Rest Aluminium und zufälligen Verunreinigungen besteht, und die Aluminiumlegierung mittels einer feinen Dispersion eisenhaltiger intermetallischer Verbindungen mit einer Größe von 5 um und weniger verfestigt wurde.
4. Hochfestes Material nach Anspruch 3, bei dem die schnell erstarrten Partikel durch Atomisieren und Erstarren einer Aluminiumlegierungsschmelze bei einer Abkühlungsgeschwindigkeit von 103 bis 104°C/sec unter Verwendung eines Gases, hergestellt wurden.
EP85110169A 1984-08-13 1985-08-13 Hochfester Werkstoff hergestellt durch Verfestigung rasch erstarrter Aluminiumlegierungsteilchen Expired EP0171798B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP167935/84 1984-08-13
JP59167935A JPS6148551A (ja) 1984-08-13 1984-08-13 高温強度に優れたアルミニウム合金成形材

Publications (2)

Publication Number Publication Date
EP0171798A1 EP0171798A1 (de) 1986-02-19
EP0171798B1 true EP0171798B1 (de) 1989-04-26

Family

ID=15858781

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EP85110169A Expired EP0171798B1 (de) 1984-08-13 1985-08-13 Hochfester Werkstoff hergestellt durch Verfestigung rasch erstarrter Aluminiumlegierungsteilchen

Country Status (4)

Country Link
US (1) US4676830A (de)
EP (1) EP0171798B1 (de)
JP (1) JPS6148551A (de)
DE (1) DE3569753D1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH673240A5 (de) * 1986-08-12 1990-02-28 Bbc Brown Boveri & Cie
US4889582A (en) * 1986-10-27 1989-12-26 United Technologies Corporation Age hardenable dispersion strengthened high temperature aluminum alloy
JPH01100233A (ja) * 1987-10-12 1989-04-18 Sumitomo Electric Ind Ltd 耐熱性アルミニウム合金及びその製造方法
FR2636974B1 (fr) * 1988-09-26 1992-07-24 Pechiney Rhenalu Pieces en alliage d'aluminium gardant une bonne resistance a la fatigue apres un maintien prolonge a chaud et procede de fabrication desdites pieces
JP2790935B2 (ja) * 1991-09-27 1998-08-27 ワイケイケイ株式会社 アルミニウム基合金集成固化材並びにその製造方法
JP2911708B2 (ja) * 1992-12-17 1999-06-23 ワイケイケイ株式会社 高強度、耐熱性急冷凝固アルミニウム合金及びその集成固化材並びにその製造方法
JP3702044B2 (ja) * 1996-07-10 2005-10-05 三菱重工業株式会社 アルミニウム合金製羽根車及びその製造方法
US9945018B2 (en) 2014-11-26 2018-04-17 Honeywell International Inc. Aluminum iron based alloys and methods of producing the same
JP2019065359A (ja) * 2017-10-03 2019-04-25 株式会社豊田自動織機 高温における機械的特性に優れたアルミニウム粉末合金製輸送機用圧縮機部品及びその製造方法
JP2019065358A (ja) * 2017-10-03 2019-04-25 昭和電工株式会社 アルミニウム合金粉末及びその製造方法、アルミニウム合金押出材及びその製造方法
JP7118705B2 (ja) * 2018-04-03 2022-08-16 株式会社豊田自動織機 高温における機械的特性に優れたアルミニウム合金製輸送機用圧縮機部品及びその製造方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0159511A1 (de) * 1984-04-04 1985-10-30 Allied Corporation Aluminium-Eisen-Vanadiumlegierungen mit hoher Festigkeit bei hohen Temperaturen

Family Cites Families (12)

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Publication number Priority date Publication date Assignee Title
CA729122A (en) * 1966-03-01 Aluminum Company Of America Aluminum alloy powder product
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
US2973570A (en) * 1958-05-13 1961-03-07 John S Nacthman High temperature structural material and method of producing same
US3380820A (en) * 1965-09-15 1968-04-30 Gen Motors Corp Method of making high iron content aluminum alloys
US3964935A (en) * 1972-04-03 1976-06-22 Southwire Company Aluminum-cerium-iron electrical conductor and method for making same
DE2946135C2 (de) * 1979-11-15 1982-09-16 Vereinigte Aluminium-Werke Ag, 5300 Bonn Verfahren zur Weiterzerkleinerung von Metallpulver
US4347076A (en) * 1980-10-03 1982-08-31 Marko Materials, Inc. Aluminum-transition metal alloys made using rapidly solidified powers and method
CA1177286A (en) * 1980-11-24 1984-11-06 United Technologies Corporation Dispersion strengthened aluminum alloys
US4464199A (en) * 1981-11-20 1984-08-07 Aluminum Company Of America Aluminum powder alloy product for high temperature application
US4743317A (en) * 1983-10-03 1988-05-10 Allied Corporation Aluminum-transition metal alloys having high strength at elevated temperatures
JPS60248860A (ja) * 1983-10-03 1985-12-09 アライド・コ−ポレ−シヨン 高温で高い強度をもつアルミニウム−遷移金属合金
FR2555610B1 (fr) * 1983-11-29 1987-10-16 Cegedur Alliages a base d'aluminium presentant une grande stabilite a chaud

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0159511A1 (de) * 1984-04-04 1985-10-30 Allied Corporation Aluminium-Eisen-Vanadiumlegierungen mit hoher Festigkeit bei hohen Temperaturen

Also Published As

Publication number Publication date
DE3569753D1 (en) 1989-06-01
EP0171798A1 (de) 1986-02-19
JPS6310221B2 (de) 1988-03-04
US4676830A (en) 1987-06-30
JPS6148551A (ja) 1986-03-10

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